FR1526647A - Advanced central body propellant nozzles - Google Patents

Advanced central body propellant nozzles

Info

Publication number
FR1526647A
FR1526647A FR5119A FR38005119A FR1526647A FR 1526647 A FR1526647 A FR 1526647A FR 5119 A FR5119 A FR 5119A FR 38005119 A FR38005119 A FR 38005119A FR 1526647 A FR1526647 A FR 1526647A
Authority
FR
France
Prior art keywords
central body
body propellant
advanced central
propellant nozzles
nozzles
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
FR5119A
Other languages
French (fr)
Inventor
Thomas Albert Wynosky
Keith Lewis Mueller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of FR1526647A publication Critical patent/FR1526647A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04—Mounting of an exhaust cone in the jet pipe

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR5119A 1966-06-01 1967-06-01 Advanced central body propellant nozzles Expired FR1526647A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US554952A US3402894A (en) 1966-06-01 1966-06-01 Base-thrust nozzles

Publications (1)

Publication Number Publication Date
FR1526647A true FR1526647A (en) 1968-05-24

Family

ID=24215382

Family Applications (1)

Application Number Title Priority Date Filing Date
FR5119A Expired FR1526647A (en) 1966-06-01 1967-06-01 Advanced central body propellant nozzles

Country Status (4)

Country Link
US (1) US3402894A (en)
DE (1) DE1626143A1 (en)
FR (1) FR1526647A (en)
GB (1) GB1194716A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3527407A (en) * 1968-07-23 1970-09-08 United Aircraft Corp Base-thrust nozzle
US3888419A (en) * 1971-09-13 1975-06-10 Thiokol Corp Spike nozzle for rockets
US3989191A (en) * 1971-09-13 1976-11-02 Thiokol Corporation Thrust control nozzle for rockets
US4168031A (en) * 1971-09-13 1979-09-18 Thiokol Corporation Thrust control nozzle for rockets
US3885385A (en) * 1972-12-22 1975-05-27 Us Army Base drag reduction
US3848806A (en) * 1973-04-30 1974-11-19 Rockwell International Corp Throttling venturi valve
US4567960A (en) * 1982-08-23 1986-02-04 The Boeing Company Fixed geometry controlled entrainment ventilated convergent nozzle and method
DE3578781D1 (en) * 1985-11-26 1990-08-23 Boeing Co SILENCER WITH FIXED GEOMETRY FOR A JET ENGINE.
US4782660A (en) * 1987-01-20 1988-11-08 Rockwell International Corporation Sequenced and pressure controlled injector
US7823376B2 (en) * 2005-09-13 2010-11-02 Aerojet-General Corporation Thrust augmentation in plug nozzles and expansion-deflection nozzles
FR2970465B1 (en) * 2011-01-19 2013-10-11 Aircelle Sa NACELLE FOR A DOUBLE FLOW AIRCRAFT AIRCRAFT TURBOREACTOR.
DE102017130568A1 (en) * 2017-12-19 2019-06-19 Rolls-Royce Deutschland Ltd & Co Kg Discharge nozzle for a turbofan engine of a supersonic aircraft

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663140A (en) * 1946-08-23 1953-12-22 Lockheed Aircraft Corp Fuel system for ram jets
US2793493A (en) * 1950-04-28 1957-05-28 Snecma Devices for deflecting fluid jets
US3048974A (en) * 1952-04-23 1962-08-14 Snecma Jet deflecting device for jet propulsion units
FR1130131A (en) * 1955-07-12 1957-01-31 Snecma Improvement in the control of stator-reactor or annular wing aerodynes
US2957307A (en) * 1956-11-06 1960-10-25 Amcel Propulsion Inc Powder propellant rocket motors
FR1268781A (en) * 1960-09-26 1961-08-04 Olin Mathieson Rocket motor and method of adjusting the thrust of a rocket motor
GB1051666A (en) * 1962-01-10 1900-01-01
US3296799A (en) * 1965-08-27 1967-01-10 Thiokol Chemical Corp Thrust vector control system

Also Published As

Publication number Publication date
US3402894A (en) 1968-09-24
GB1194716A (en) 1970-06-10
DE1626143A1 (en) 1970-09-24

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